FAMILIA

ATA 00-20. Airplane General 1.What is the center forward panel?. P1 panel. P2 panel. P3 panel.

ATA 31. Indicating and Recording System 2.What does AIMS stand for?. Airplane Information and Monitoring System (AIMS). Airplane Information Managment System (AIMS). Aircraft Information Managment System (AIMS).

ATA 24. Electrical Power 3. What are the stanby sources?. Runway Air turbine (RAT) and main battery. Radar Altimeter Transmitter (RAT) and main battery. Ram Air Turbine (RAT) and main battery.

ATA 51-57 Airframe Structure 4. What type of door is the passenger door?. Non plug type. Plug type. Type A+.

ATA 46. Information system 12. What does EFB stand for?. Electronic Flight Bag. Electrical Flight Bag. Electronic Function Bag.

ATA 47. NGS 13. What are the NGS operation modes?. Operates only in a one mode, high flow. Operates in three flow modes, low flow, intermedium flow, and high flow. Operates in two modes, low flow and high flow.

ATA 49. APU 14. At what altitude can the APU supply electrical power?. 22,000 ft (6,700m). 41,000 ft (12,4979m). All altitudes.

ATA 33. Lights 15. How many logo lights are installed in the B777?. 6 logo lights. 4 logo lights. 2 logo lights.

ATA 34. Navegation 16. The standby attitude reference system has a integrated standby flight display (ISFD) that shows: Attitude, Auto Thrust, Altitude. Latitude Airspeed, Altitude. Attitude, Airspeed, Altitude.

ATA 34. Navegation 17. Where is located the Integrated Standby Flight Display?. The ISFD is on the P1-2 panel in the flight compartment. The ISFD is on the P3-1 panel in the flight compartment. The ISFD is on the P2-1 panel in the flight compartment.

ATA 29. Hydraulic System 19. The components and hydraulic tubing of the three systems are color coded. How is identify each system?. The left system is yellow, the center system is blue, an the right system is green. The left system is red, the center system is blue, and the right system is yellow. The left system is red, the center system is blue, and the right system is green.

ATA 22. Auto flight 20. How is the MCP attached to the glareshield structure?. With four tie-wraps. with four screws. With four studs.

ATA 26. Fire Protection 21. How many fire extinguisher bottles does the engine system have?. 1. 2. 4.

ATA 21. Air conditioning 18. What mode can each outlet valve operate in?. Automatic or manual mode equal to the mode set for the other valve. Upper and Lower. Automatic or Manual Mode independent of the mode set for the other valve.

ATA 23. Communication 22. How many Zone Managment Units (ZMU) are there?. Four. Five. Six.

ATA 36. Pneumatics 23 The Pneumatics system supplies air from one of these sources to the user systems. Engines, Auxiliary Power Unit (APU), Ground Air. Engine, Power Transfer Unit (PTU), Nitrogen Generating System (NGS). None of the above.

ATA 27, Flight Control 24. Which are the components that the PCU's consist of?. A hydraulic actuator, an electrohydraulic servo valve, two position feedback transducer. A hydraulic actuator, an electrohydraulic servo valve, A position feedback transducer. A hydraulic actuator, two electrohydraulic servo valve, A position feedback transducer.

ATA 27. Flight Control 25. What are there three modes of operation of the HLCS?. Primary, Secondary and Alternate. Primary, Main and Alternate. Primary, Secondary and Direct.

ATA 32 Landing Gear 26. In which moment will the main gear steering operate?. When the NLG turns more than 6.5 degrees. When the NLG turns more than 13 degrees. When the NLG turns less than 13 degrees.

ATA 32 Landing Gear 26. From which Hydraulic system takes power the normal braking system?. From the left hydraulic system. From the right hydraulic system. From the center hydraulic system.

ATA 30, Ice and Rain Protection 28. What are the probes and sensors that have heaters?. Left, Right and center pitot probes, Total air temperature (TAT) probe, Left and right angle of attack (AOA) sensors. Only left pitot probes, Total air temperature (TAT) probe, Only Left angle of attack (AOA) sensors. Left, right,and center static ports, Total air temperature (TAT) probe, Left and right angle of attack (AOA) sensors.

ATA 70.80 (GE 90) 29. Which shaft is connected to the accesory gear box (AGB)?. N1. N3. N2.

ATA 70-80 (GE90) 30. Where does the engine Primary airflow go through?. Compressors, combustion section and turbines. Engine Core. Engine Inlet, LPT, Exhaust.

ATA 70-80 (GE90) 31. Where is located the HMU?. MEC. Accesory Gear box. Engine Pylon.

ATA 70-80 (GE90) 32. Where is the AGB located?. Below the high-pressure compressor. Upper the high-pressure compressor. Ride side of engine.

ATA 70-80 (RR Trent 800) 33. What is EPR?. Ratio of turbine exahust pressure to Fan inlet pressure. Ratio of compressor Inlet Temperature to Exhaust gases. Ratio of turbine exhaust to Low pressure compressor.

ATA 70-80 (RR Trent 800) 34. Where does the engine primary airflow go through?. Compressors, combustion section, and turbines. Compressors, Core and Turbine. Engine Inlet, LPT, Exhaust.

ATA 70-80 (RR Trent 800) 35. How many spark plugs does the engine ignition system?. 4 Ingniter plugs. 3 Ingniter Plugs. 2 Ingniter Plugs.

ATA 70-80 (RR Trent 800) 36. Whats the meaning of OPU?. Overthrust Prevent Unit. Overrated Protection Unit. Overspeed Protection Unit.

ATA 70-80 (PW4000) 37. What is the Engine Bypass Ratio (PW4000)?. 8:5. 5:2. 6-4:1.

ATA 70-80 (PW4000) 38. Where is the Engine data plate located?. Left side of the main gear box. Right side of the ENGINE. Left side of the low-pressure compressor.

ATA 70-80 (PW4000) 39. Where are located all engine control components?. P10 Control Stand. P8 Aft aisle stand panel. P9 Forward aisle stand panel.

ATA 70-80 (PW4000) 40. What is the primary component of the engine fuel control system?. PMA. FMU. EEC.